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R Handle Flap Mechanism Assy
R Figure 606/TASK 52-31-11-991-028
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R -------------------------------------------------------------------------------
R | FIG. | ORIGINAL MANUFACTURING LIMITS | IN-SERVICE WEAR LIMITS |
R | DETAIL |---------------------------------------|----------------------------|
R | AND | DIMENSION | ASSEMBLY CLEARANCE| DIMENSION LIMITS | MAX. |
R | ITEM | MM (IN.) | MM (IN.) | MM (IN.) | ALLOW. |
R | NO. |-------------------|-------------------|---------|---------| CLEAR. |
R | | MIN. | MAX. | MIN. | MAX. | MIN. | MAX. |MM (IN.)|
R |--------|---------|---------|---------|---------|---------|---------|--------|
R | D-D | 6.336 | 6.345 | | | 6.323 | | |
R | OD 3 |(0.2494) |(0.2498) | | |(0.2489) | | |
R | | | | 0.005 | 0.029 | | | 0.063 |
R | | | | (0.0001)| (0.0011)| | |(0.0024)|
R | D-D | 6.350 | 6.365 | | | | 6.386 | |
R | ID 4 |(0.2500) |(0.2505) | | | |(0.2514) | |
R -------------------------------------------------------------------------------
R Subtask 52-31-11-220-062
R E. Measurement of the Hinge Pins and the Piano Hinges
R (Ref. Fig. 607/TASK 52-31-11-991-029)
R -------------------------------------------------------------------------------
R | FIG. | ORIGINAL MANUFACTURING LIMITS | IN-SERVICE WEAR LIMITS |
R | DETAIL |---------------------------------------|----------------------------|
R | AND | DIMENSION | ASSEMBLY CLEARANCE| DIMENSION LIMITS | MAX. |
R | ITEM | MM (IN.) | MM (IN.) | MM (IN.) | ALLOW. |
R | NO. |-------------------|-------------------|---------|---------| CLEAR. |
R | | MIN. | MAX. | MIN. | MAX. | MIN. | MAX. |MM (IN.)|
R |--------|---------|---------|---------|---------|---------|---------|--------|
R | B-B | 10.857 | 10.900 | | | 10.400 | | |
R | OD 1 |(0.4274) |(0.4291) | | |(0.4094) | | |
R | | | | 0.300 | 0.386 | | | 1.100 |
R | | | | (0.0118)| (0.0151)| | |(0.0433)|
R | B-B | 11.200 | 11.243 | | | | 11.500 | |
R | ID 2 |(0.4409) |(0.4426) | | | |(0.4527) | |
R -------------------------------------------------------------------------------
R 5. Close-up________
R Subtask 52-31-11-860-064
R A. Put the aircraft back to the serviceable condition.
R (1) Make sure that the FWD cargo compartment door (referred to as cargo
R door) is closed and locked (Ref. TASK 52-30-00-860-001).
R (2) Install the access panel 825AR on the cargo door.
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R Door Hinge
R Figure 607/TASK 52-31-11-991-029
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R (3) Assemble the locking handle mechanism (Ref. TASK 52-31-21-400-001).
R (4) Install the handle flap mechanism on the cargo door (Ref. TASK 52-31-
R 21-000-002).
R (5) Connect the FWD and/or AFT cargo door hinge (Ref. TASK 52-31-11-400-
R 002).
R (6) Remove the crane from the cargo door (Ref. TASK 52-31-11-400-002).
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TASK 52-31-11-200-011
General Visual Inspection of Forward Cargo Compartment Door Skin, External Surface
1. Reason for the Job
__________________
Refer to the MPD TASK: 523101-01
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific 1 ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE
B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION
-------------------------------------------------------------------------------
ASRM 52310010100
ASRM 51730010100 (for corrective action)
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